General Information
    • ISSN: 2010-0221
    • Frequency: Bimonthly
    • DOI: 10.18178/IJCEA
    • Editor-in-Chief: Prof. Dr. Shen-Ming Chen
    • Executive Editor: Mr. Ron C. Wu
    • Abstracting/ Indexing: Chemical Abstracts Services (CAS), Ulrich's Periodicals Directory, CABI, Electronic Journals Library, Google Scholar, ProQuest, and Crossref
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Prof. Dr. Shen-Ming Chen
National Taipei University of Technology, Taiwan

IJCEA 2010 Vol.1(4): 319-325 ISSN: 2010-0221
DOI: 10.7763/IJCEA.2010.V1.55

CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1

K. M. Pandey, Member, IACSIT and S. K. Yadav

Abstract—In this paper CFD analysis of pressure and temperature for a rocket nozzle with four inlets at Mach 2.1 is analyzed with the help of fluent software. when the fuel and air enter in the combustion chamber according to the x and y plot, it is burning due to high velocity and temperature and then temperature increases rapidly in combustion chamber and convergent part of the nozzle and after that temperature decreases in the exit part of the nozzle. it is concluded in this paper that Four inlet rocket nozzle is having better performance than single inlet and two inlet as seen from the previous research work done.

K. M. Pandey, Member IACSIT, Department of Mechanical Engineering, N.I.T Silchar, Assam, India (email:
S. K. Yadav, Asst. Professor, Department of Mechanical Engineering,Gurgaon Engineering College, Gurgaon.


Cite: K. M. Pandey and S. K. Yadav, "CFD Analysis of a Rocket Nozzle with FourInlets at Mach 2.1," International Journal of Chemical Engineering and Applications vol. 1, no. 4, pp. 319-325, 2010.

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